The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Jul. 28, 2015

Filed:

Jun. 11, 2012
Applicants:

Dominic A. Waldron, Swadlincote, GB;

Peter Beardsley, Derby, GB;

Inventors:

Dominic A. Waldron, Swadlincote, GB;

Peter Beardsley, Derby, GB;

Assignee:

ROLLS-ROYCE PLC, London, GB;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 29/06 (2006.01); F02C 7/20 (2006.01); B64D 27/26 (2006.01);
U.S. Cl.
CPC ...
B64D 29/06 (2013.01); B64D 27/26 (2013.01); F02C 7/20 (2013.01); B64D 2027/262 (2013.01); B64D 2027/264 (2013.01); B64D 2027/266 (2013.01); Y02T 50/44 (2013.01);
Abstract

A mounting assembly for attaching a ducted fan gas turbine engine that includes an intake, a propulsive fan, a fan case surrounding the fan, and a core engine. The air intake is attached to the front of the fan case such that loads acting on the air intake are transmitted to the fan case. The mounting assembly includes: a support structure extending in an axial direction of the engine and having a rearward region adapted to attach to the aircraft; and a load distribution ring coaxial with and rearward of the fan case, adapted to join to the fan case, and joined to a forward region of the support structure. The support structure and the load distribution ring are adapted such that the primary load path for the loads transmitted to the fan case by the air intake is through the load distribution ring and the support structure.


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